The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman

The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analysis uses a real model of aircraft structure courtesy of the SME Aviation Sdn. Bhd. which is located at Subang, Selangor Darul Ehsan. This final project focuses more onto the structural analysis compar...

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Main Author:	Abdul Rahman, Wan Arma Idayu
Format:	Thesis
Language:	English
Published:	2002
Subjects:	Stability of airplanes, Longitudinal Oscillations Damping Aircraft
Online Access:	https://ir.uitm.edu.my/id/eprint/21248/1/TD_WAN%20ARMA%20IDAYU%20ABDUL%20RAHMAN%20EM%2002_5.pdf
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id	my-uitm-ir.21248
record_format	uketd_dc
spelling	my-uitm-ir.212482018-10-11T08:18:20Z The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman 2002 Abdul Rahman, Wan Arma Idayu Stability of airplanes, Longitudinal. Oscillations. Damping Aircraft The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analysis uses a real model of aircraft structure courtesy of the SME Aviation Sdn. Bhd. which is located at Subang, Selangor Darul Ehsan. This final project focuses more onto the structural analysis compared to the aerodynamic. In order to complete this analysis, several steps have to be done and that include literature review, field visit, theoretical analysis, finite element analysis and result compilation and discussion. In literature review, few books were taken as an example and this step is done in order to strengthen the knowledge of Strength of Material and as an introduction to aerodynamic theory while field visit makes the understandings of aircraft wing structure more comprehendible and enjoyable. The analysis begins with the calculation of aircraft loading in order to find the lift distribution, and bending- moment value. Stress analysis is done next and this analysis is more tedious as it focuses more on the wing structure. The deflection of the wing is found next and the theoretical analysis is hence, completed. The second part of the analysis is the execution of finite element analysis using ANSYS and the comparison of result between the theoretical analysis and finite element analysis is made. 2002 Thesis https://ir.uitm.edu.my/id/eprint/21248/ https://ir.uitm.edu.my/id/eprint/21248/1/TD_WAN%20ARMA%20IDAYU%20ABDUL%20RAHMAN%20EM%2002_5.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
topic	Stability of airplanes, Longitudinal Oscillations Damping Aircraft
spellingShingle	Stability of airplanes, Longitudinal Oscillations Damping Aircraft Abdul Rahman, Wan Arma Idayu The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
description	The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analysis uses a real model of aircraft structure courtesy of the SME Aviation Sdn. Bhd. which is located at Subang, Selangor Darul Ehsan. This final project focuses more onto the structural analysis compared to the aerodynamic. In order to complete this analysis, several steps have to be done and that include literature review, field visit, theoretical analysis, finite element analysis and result compilation and discussion. In literature review, few books were taken as an example and this step is done in order to strengthen the knowledge of Strength of Material and as an introduction to aerodynamic theory while field visit makes the understandings of aircraft wing structure more comprehendible and enjoyable. The analysis begins with the calculation of aircraft loading in order to find the lift distribution, and bending- moment value. Stress analysis is done next and this analysis is more tedious as it focuses more on the wing structure. The deflection of the wing is found next and the theoretical analysis is hence, completed. The second part of the analysis is the execution of finite element analysis using ANSYS and the comparison of result between the theoretical analysis and finite element analysis is made.
format	Thesis
qualification_level	Bachelor degree
author	Abdul Rahman, Wan Arma Idayu
author_facet	Abdul Rahman, Wan Arma Idayu
author_sort	Abdul Rahman, Wan Arma Idayu
title	The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
title_short	The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
title_full	The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
title_fullStr	The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
title_full_unstemmed	The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman
title_sort	analysis of sme md3 - 160 aircraft wing structure / wan arma idayu abdul rahman
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2002
url	https://ir.uitm.edu.my/id/eprint/21248/1/TD_WAN%20ARMA%20IDAYU%20ABDUL%20RAHMAN%20EM%2002_5.pdf
_version_	1783733748914716672

The analysis of SME MD3 - 160 aircraft wing structure / Wan Arma Idayu Abdul Rahman

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